Classifications

• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64C—AEROPLANES; HELICOPTERS
  • B64C39/00—Aircraft not otherwise provided for
  • B64C39/02—Aircraft not otherwise provided for characterised by special use
  • B64C39/026—Aircraft not otherwise provided for characterised by special use for use as personal propulsion unit
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
  • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
  • B63B34/00—Vessels specially adapted for water sports or leisure; Body-supporting devices specially adapted for water sports or leisure
  • B63B34/10—Power-driven personal watercraft, e.g. water scooters; Accessories therefor
  • B63B34/15—Power-driven personal watercraft, e.g. water scooters; Accessories therefor for hydroflight sports
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
  • B63H—MARINE PROPULSION OR STEERING
  • B63H11/00—Marine propulsion by water jets
  • B63H11/02—Marine propulsion by water jets the propulsive medium being ambient water
  • B63H11/04—Marine propulsion by water jets the propulsive medium being ambient water by means of pumps
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64C—AEROPLANES; HELICOPTERS
  • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
  • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
  • B64C15/12—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets the power plant being tiltable
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64C—AEROPLANES; HELICOPTERS
  • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
  • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
  • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
  • B64C29/0075—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors the motors being tiltable relative to the fuselage
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
  • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
  • B64D27/02—Aircraft characterised by the type or position of power plants
  • B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
  • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
  • B64D27/02—Aircraft characterised by the type or position of power plants
  • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
  • B64D37/00—Arrangements in connection with fuel supply for power plant
  • B64D37/02—Tanks
  • B64D37/06—Constructional adaptations thereof
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
  • B63H—MARINE PROPULSION OR STEERING
  • B63H11/00—Marine propulsion by water jets
  • B63H2011/006—Marine propulsion by water jets with propulsive medium supplied from sources external to propelled vessel, e.g. water from public water supply
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
  • Y02T50/00—Aeronautics or air transport
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
  • Y02T50/00—Aeronautics or air transport
  • Y02T50/30—Wing lift efficiency
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
  • Y02T50/00—Aeronautics or air transport
  • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Definitions

• the invention relates to a device for propelling a passenger so that the latter can move in the air with very great freedom of movement thanks to his agility and his physique.
• the invention further provides that the device is very simple to implement and accessible to the greatest number.
• a propulsion device was developed in the sixties of the last century, as described in US 3,243,144 or US 3,381,917 .
• a propulsion device comprises a body in the form of a harness or a seat against which or in which a passenger can take place.
• a body cooperates with a thrust group, in particular in the form of a pair of nozzles, to eject a pressurized fluid and thus generate a pushing force sufficient to sustain the passenger in the air.
• the nozzles are clearly arranged above the center of gravity of the body-passenger, more specifically at the shoulders of the passenger.
• the thrust unit further comprises a fluid compression station supplied with gas or flammable liquid (s) and positioned in the passenger's back. This station is able to sufficiently feed the nozzles to cause the takeoff of the passenger transformed in some way into a human rocket.
• a fluid compression station supplied with gas or flammable liquid (s) and positioned in the passenger's back. This station is able to sufficiently feed the nozzles to cause the takeoff of the passenger transformed in some way into a human rocket.
• the low autonomy and dangerousness of such devices have kept them in relative confidentiality.
• the configuration of the nozzles above the center of gravity of the device gives the impression of the passenger to be suspended at the level of the shoulders by a virtual crane hook and thus deprived him of many sensations caused by falls, figures of improvised or acrobatic styles.
• the variety of directions and movements is limited. It is not easy, for example, to move "in crab” with a known device, or even to instantly move from a straight trajectory on the surface of the water to a diving phase followed by multiple displacements under the surface of the water. 'water.
• FIG. 1 thus shows an embodiment of such a propulsion device 10.
• This device 10 comprises a main body in the form of a substantially flat platform 11 on which a passenger 1 can take place.
• the propulsion device described in connection with FIG. 1, comprises a thrust group cooperating with the platform 11.
• Such a thrust unit consists of a pair of main nozzles 12a and 12b fixed against the underside of the platform 11.
• the thrust group of such a device may further comprise two secondary nozzles 13a and 13b to facilitate its maneuverability.
• the device 10 also comprises means for collecting and delivering a fluid under pressure, for example water, to the main and secondary nozzles.
• a fluid under pressure for example water
• Such a fluid is preferably conveyed by means of a flexible supply duct 2 from a remote compression station, not shown in FIG. 1.
• a supply duct can be made from a fire hose or all other materials having the necessary resistance to the pressure exerted by the fluid under pressure.
• a collector 14y can thus have a base 14c to which is connected a tip 2a of a supply duct 2, for example by means of a groove adapted to receive said duct 2.
• the collector 14y can present a shape close to a "Y" to collect from the base 14c and distribute via the arms the fluid under pressure respectively to the main nozzles 12a and 12b.
• the collector 14y is connected to the main nozzles or via an optional bend 15, in order to orient the main nozzles along an axis substantially perpendicular to the underside of the platform 11.
• the arms are connected to said main nozzles via said elbow 15, according to a pivot connection at the arms.
• Such an arrangement allows free rotation along an axis F substantially parallel to the arms of the collector 14y.
• said collector can describe a quasi-free rotation rl about said axis F, modulo the stop that represents the underside of the platform 11 at an excessive inclination thereof.
• Such a pivot connection allows the user to "take off” easily from the surface of the water and gives it a great ability of orientation and movement.
• a relative rotation of the collector around the axis F with respect to the plane of the lower face of the platform 11, consecutive rotation of the connection of the collector with the supply duct 2, does not cause rotation of the platform 11.
• the tip 2a of the supply duct 2 can advantageously cooperate with the collector 14y at its base 14c in a pivot connection to allow a free rotation r2 about an axis C substantially parallel to the duct 2.
• the device can thus freely pivot about said axis C without generating loops or excessive stress on the supply duct 2.
• secondary ducts 18a and 18b - in the advantageous form of flexible hoses - may be provided to deliver from the collector 14y said fluid under pressure at the secondary nozzles.
• said secondary ducts can be guided along the back to the shoulders by the use of holding means 19, such as straps, harnesses, etc.
• a passenger may further use means to constrain the secondary nozzles at his forearms.
• the platform 11 may have means for holding a passenger on the upper face of said platform 11.
• said holding means may consist - as indicated in FIG. in a pair of slippers, foot straps, also known by the Anglo-Saxon name “Foot Straps”, or fastening boots 16 of a type similar to what can be found, for example, in the wakeboarding practice.
• a propulsion device such as the device 10 described in connection with FIG. 1, can be powered by any fluid compression station at from the moment when it is able to deliver a fluid whose pressure is sufficient to ensure the operation of the propulsion device. It can be remote and dedicated to this use at the risk of increasing the overall cost of a propulsion system comprising a propulsion device, a compression station and a supply duct cooperating with said device and station to route the device. fluid under pressure.
• a station may alternatively consist of using a motorized nautical vehicle (hereinafter referred to as "VNM”) adapted, as described in document WO2013 / 041787A1, to reduce costs.
• VNM motorized nautical vehicle
• Figure 1 preferably describes a system in which the fluid used is water under pressure to move on the surface of the water.
• the propulsion device described in connection with Figure 1 allows to move easily in and / or on the surface of the water and offers the user very large degrees of freedom to achieve a large number of figures, it can present, for some, some disadvantages.
• the nozzles are supplied with compressed fluid, in particular water, conveyed to the device by means of a conduit via a collector, connecting said device to a fluid compression station advantageously distant.
• compressed fluid in particular water
• a conduit via a collector
• a fluid compression station advantageously distant.
• a floating compression station on said body of water for example a motorized watercraft adapted to cooperate with said conduit at the fluid outlet, collects water, compresses it by turbining and delivers it via the conduit.
• the invention makes it possible to achieve such an objective, thus solving the disadvantages of the known solutions.
• New perspectives on passenger travel and entertainment are thus within everyone's reach. Only the autonomy remains to be possibly increased according to the envisaged application.
• the development of technologies, particularly in terms of thrusters or batteries, will only confirm the relevance of a propulsion device for a passenger according to the invention.
• the arrangement of such a device guarantees such reliability that the passenger can keep his device operational, even if the thrust unit of said device is partially defective;
• a device for propelling a passenger comprising a body having a platform arranged to accommodate said passenger and a push group.
• said thrust group comprises at least two thrust subgroups each comprising at least one thruster
• Each thruster is steerable along an axis substantially normal to a longitudinal plane of the platform, the ejection nozzle of each of said thrusters rejecting a gas flow in a direction opposite to that of a longitudinal axis oriented from the feet to the passenger's head ;
• said body of the device comprises support means of the thrust group cooperating with the platform and being arranged to support said thrust group and to minimize the distance between a median axis passing through the center of gravity of the device body and the direction of ejection of gas flow through the ejection nozzle of each thruster.
• each of said thrust subgroups may comprise at least two thrusters.
• the platform can be arranged so that the feet of the passenger occupy a position whose relative height at the low point of the device, when said passenger occupies a substantially vertical position and that the nozzles thrusters are directed towards the ground, is:
• the body of the latter may comprise projecting means cooperating with the platform and arranged to prevent any shock or direct contact between the ground and the thrust unit of the device.
• one of said thrusters may be a propeller propeller.
• one of said thrusters may be a turbojet engine.
• thrusters of the thrust group may be arranged counter-rotating.
• the support means may be arranged to keep the thrusters of each thrust subgroup parallel, or even to orient the direction of ejection of gas flow by the ejection nozzle of each thruster of each sub-unit. thrust group for said gas flow ejection direction to describe an angle between -10 ° and + 10 ° with a median axis of the platform.
• a propulsion device may comprise a fairing cooperating with the platform or constituting with said platform the same physical entity, arranged to prevent any direct contact between the thrust unit and the passenger .
• said fairing may comprise a gate arranged to partially obscure the fluid inlets of thrusters of the thrust unit and thus prevent the aspiration of foreign bodies by said fluid inlets.
• the propellant support means can cooperate with secondary support means to cooperate with secondary propellants and maintain the latter in an orientation substantially parallel to a longitudinal axis of the platform.
• the latter may advantageously furthermore comprise:
• a reservoir of a fuel selected to feed thrusters of the thrust group said reservoir cooperating with the platform or the passenger;
• a collector cooperating with the thrust unit arranged to distribute said fuel to thrusters of the thrust group;
• the latter can comprise a human-machine interface of instructions translating a gesture of the passenger into an instruction, means of said setpoint generated and generating a power control thrusters from said setpoint produced, said thruster power control being conveyed to the thrust group by communication means.
• Such a propulsion device may further comprise a trim sensor and / or trajectory cooperating with the body of the device substantially at the position of the center of gravity of the latter and with the processing means, the latter generating the power control thrusters from information provided by the attitude sensor and / or trajectory together with a setpoint produced by the man-machine interface.
• the processing means present on the body of the device when the latter comprises secondary thrusters, can generate power commands of said secondary thrusters from information supplied by the attitude and / or trajectory sensor for actuating one of said secondary thrusters and maintaining the current trajectory of said body, in the absence of a command produced by the 'Human Machine Interface.
• such a man-machine setpoint interface may include a trigger operable by one or more fingers of the passenger.
• the processing unit can then develop a power control thrusters to regulate the power developed by the thrust group according to the stroke of said trigger.
• said man-machine setpoint interface may comprise an angular measurement sensor measuring the angle described by a wrist of the passenger with respect to the longitudinal axis of the forearm concerned relative to a reference position in which the passenger's hand is aligned with said forearm.
• the processing unit can therefore develop a power control secondary thrusters to regulate the power developed by them according to the wrist race.
• the latter can advantageously include means for maintaining said passenger on the platform.
• FIG. 1 already described, shows a device for propelling a passenger using a fluid compressed by a remote compression station according to the prior art
• FIG. 2A, 2B and 2C describe an embodiment of a passenger propulsion device according to the invention
• FIG. 3 depicts an exploded view of an embodiment of such a propulsion device according to the invention, thus presenting the main elements of the body of such a passenger propulsion device;
• FIG. 4 presents in detail an exemplary embodiment of a thrust unit of a device according to the invention
• FIG. 5 depicts an example of a fuel tank for supplying the thrust unit of a device according to the invention
• FIG. 6 describes an exemplary embodiment of a human-machine interface for transmitting instructions from the passenger to the control member of the thrust unit of a device according to the invention.
• Figure 2A shows a perspective view of a preferred embodiment of a propulsion device 10 of a passenger 1 according to the invention.
• a device 10 comprises a main body 10a in the form mainly of a platform 11 on which a passenger 1 can take place.
• the invention provides that several passengers can possibly take position simultaneously on said platform 11.
• the platform 11 has, as such, one or more beaches lia arranged to accommodate the feet or shoes of the passenger 1, as indicated more particularly in particular Figure 3.
• Such beaches 11a may include means 16 for holding the passenger 1 on the platform 11.
• said Retaining means 16 may consist of a pair of booties or boots of a type similar to what can be found, for example, in the practice of wakeboarding.
• Other types of holding means could be preferred, depending on whether it is desired to maintain a passenger in the "bent legs", kneeling or even sitting position.
• Such a platform 11 can be advantageously made from one or more materials having alone or in combination sufficient rigidity to support the weight of the passenger or passengers and thus prevent excessive deformation.
• the body 10a of the propulsion device 10 described in connection with Figures 2A and 3 comprises a thrust group 12 cooperating with the platform 11. Such a group 12 is described later in connection with Figure 4 in particular.
• Transverse plane PT any plane normal to a median plane, which separates the body 10a of the propulsion device 10 into two halves, one having the front, and the other comprising the rear of said body, said halves not necessarily equal;
• Longitudinal plane PL any plane normal to transverse and median planes, said longitudinal plane separating an upper half of a lower half of the body 10a of the device 10, said halves not necessarily being equal.
• Transverse axis means any axis belonging both to a transverse plane and to a longitudinal plane;
• longitudinal axis means any axis belonging both to a median plane and to a longitudinal plane
• Median axis means any axis belonging to both a median plane and a transverse plane.
• a propulsion device 10 comprises other accessory elements, not represented as a simplification measure in FIG. 2A, such as a fuel tank for supplying the thrust unit 12 or a human-machine interface, such as a remote control, so that the passenger 1 can interact with the thrust group 12 of said device 10.
• accessory elements not represented as a simplification measure in FIG. 2A, such as a fuel tank for supplying the thrust unit 12 or a human-machine interface, such as a remote control, so that the passenger 1 can interact with the thrust group 12 of said device 10.
• Such accessories will respectively be described in conjunction with FIGS. 5 and 6.
• FIGS. 2B and 2C describe such a propulsion device 10 according to the invention, respectively of profile and of face.
• the body 10a of such a device 10 comprises projecting means 17 cooperating with the platform 11 and arranged to prevent any shock or direct contact between the ground and the group of
• Such means 17 may consist in particular of four feet of lengths sufficient for the ejection nozzle or nozzles of the thrust group 12 not to strike the ground and also to offer a certain stability, when the device is on the ground or on a take-off station, not shown in FIGS. 2A to 2C, so that the passenger can take an effective position on the platform 11.
• such means 17 could consist of a pair of skis or any other suitable elements. to ensure a certain stability according to the nature of the ground or the support of the device.
• Figure 3 shows an exploded view of a body 10a of such a device 10 according to the invention.
• the thrust group 12 advantageously consists of a pair of thrust subgroups 12a and 12b each comprising two thrusters.
• a first thrust subgroup 12a has two 12al and 12a2 thrusters.
• the thrust subgroup 12b which comprises two thrusters 12bl and 12b2.
• the thrust unit 12 could comprise more thrust subgroups, themselves comprising one or more thrusters.
• a device 10 could evolve with a thrust group reduced to a single propeller, for example of the thermal turbojet type.
• this configuration would have a size too large to allow the passenger 1 to be able to move easily as if he was moving on a Flyboard.
• the length of such a single thruster so that the latter is able to deliver a thrust sufficient to propel the device 10 and its passenger 1, would be of the order of one meter or more .
• a thrust group 12 comprising two subgroups comprising only one thruster each.
• the size of each propellant would be reduced, but such a pusher assembly 12 retain a major drawback in terms of safety, as the configuration mono ⁇ propellant previously expressed. Indeed, if one of the two thrusters was to malfunction, the total thrust of the group would be insufficient to maintain the passenger 1 in the air and to maintain sufficient maneuverability.
• a configuration as illustrated in connection with FIGS. 3 and 4, according to which a thrust group 12 comprises at least two thrust subgroups 12a. and 12b each comprising at least two thrusters 12al and 12a2 for one and 12bl and 12b2 for the other, offers a particularly interesting compromise.
• the space caused by the four thrusters, for example reactors remains fully compatible with the desired terms of use.
• the propulsion device 10 remains perfectly manoeuvrable, even if one of the thrusters was to malfunction.
• the thrusters of the thrust group 12 are advantageously positioned as centrally as possible of the body 10a of the device 10.
• the lia beaches arranged on the platform 11 to accommodate the feet or shoes of the passenger 1 will advantageously positioned on either side of said thrust group 12. This reduces the moment of inertia that the passenger must overcome to change to using his body the plate of the device 10 and thus move:
• the thrust group 12 may advantageously comprise two secondary thrusters. 19a and 19b. These are advantageously arranged eccentrically along a transverse axis of the platform. By being actuated non-simultaneously, these thrusters respectively create a sufficient torque to cause a curved trajectory.
• the invention provides to be able to add to all or part of thrusters or thrust subgroups 12a, 12b an output of orientable fluid, of the steerable cone type of a fluid outlet of a jet ski for example, which would cooperate with the ejection nozzle of the gas flow of the propellant or propellers concerned, according to one or the respective mechanical links adapted, such as for example links pivot or recess.
• support means 14 constitute the functional equivalent of a chassis supporting the platform 11 and cooperating according to FIG. an advantageous link which does not have a degree of freedom or connection with the projecting means 17 conferring a seat and a protection of the thrust unit 12 of such a device 10.
• the body 10a of a propulsion device 10 may comprise a fairing 13u, cooperating with the platform 11, by any reversible or irreversible mechanical connection (welding, screwing, for example) or constituting with said platform 11 the same physical entity.
• the function of such a fairing 13u is to prevent any direct contact between the thrust group 12 and the passenger 1.
• the morphology (dimensions, shape) of such fairing 13u will thus be arranged to adapt to the dimensions of the group of thrust 12, provide an aesthetic and / or treat the aerodynamics of the propulsion device, while limiting any inconvenience to the passenger.
• the temperature of the outer walls of the thrust group 12 can quickly be very high.
• the upper part of the body 10a of the device 10 located substantially between the feet of the passenger comprises a fluid inlet 18, in this case an inlet of air, to supply fluid to the thrusters via the respective fluid inlets thereof.
• the thrusters comprise rotors capable of injuring the passenger 1 if the passenger inserts a hand into the fluid inlet 18 inadvertently.
• the suction of foreign elements (leaves, debris, volatile, etc.) by said fluid inlet 18 could alter the operation of the thrust unit 12.
• said fairing 13u may advantageously comprise a grid , not shown in Figure 3, the configuration allows to partially obscure said inlet 18 and thus limit or prevent the aspiration of foreign bodies by said air inlet 18 while preserving the fluid exchange between the outside world and the thrusters .
• FIG. 3 furthermore describes the operation of a lower fairing 13d, cooperating by means of any mechanical connection by embedding, also ensuring a protective function of the passenger or of the environment close to the fluid outlets or jet nozzles.
• gas thrusters thrust subgroups 12a and 12b.
• the temperature can indeed be particularly high in the direct vicinity of said exhaust nozzles.
• Such a fairing open allows for circumferential or lateral protection.
• the geometry of such a fairing 13d can also be advantageously determined so as not to alter the gas ejection of the thrust unit and improve the aerodynamics of the body 10a. of the device 10.
• the choice of the material or materials provided to form such fairings 13u and 13d will be a function of the maximum temperature of the thrust group 12 in the direct vicinity of said fairings so that it does not alter the structure of the latter.
• FIG. 3 also describes the presence of secondary thrusters 19a and 19b located laterally and non-centrally, unlike the thrust subassemblies 12a and 12b. We will describe the contribution of such secondary thrusters in connection with the detailed presentation of an example of thrust group illustrated in Figure 4.
• the body 10a of a propulsion device 10 in accordance with the invention comprises means for processing passenger instructions for control the power of the thrusters.
• processing means may further cooperate or include sensors, such as non-exhaustively an inclinometer, accelerometer and / or gyroscope, capable of delivering information related to the plate or more generally the trajectory of the body 10a of the device 10.
• Said processing means are thus arranged to develop power controls thrusters of the thrust group 12, including thrusters thrust subgroups 12a and 12b, according to the instructions of the passenger and / or information produced by such sensors.
• Such processing means may be in the form of one or more electronic cards, advantageously positioned near the center of inertia CG10 of the body 10a of the propulsion device 10, especially if the sensors are included in said electronic card or cards.
• FIG. 2C illustrates in particular the virtual position of said CG10 center of gravity of the body 10a of the exemplary embodiment of the propulsion device 10.
• 12 comprises two thrust subgroups 12a and 12b each comprising two thrusters, referenced 12al and 12a2 for the first, and 12bl and 12b2 for the second.
• Such thrusters may consist of thrusters propellers or rotors, or advantageously, and in this case as shown in Figure 4, in turbojet engines.
• a turbojet is a thermal engine, commonly used in aeronautics, which transforms the potential energy contained in a fuel, for example kerosene or equivalent, associated with an oxidant, in this case the ambient air sucked by the fluid inlet. 18 of the body 10a, in kinetic energy. This kinetic energy generates a reaction force in an elastic medium, in the opposite direction to the ejection of a gas discharge. This results in an acceleration of a certain amount of air between the fluid inlet of the propellant and the ejection nozzle of the latter, producing an expansion thrust in said ejection nozzle.
• Such a thruster uses a paddle or rotor air compressor. Any other type of fuel could possibly be used in place of the kerosene mentioned above.
• each thruster of the thrust subgroups 12a and 12b is steerable and, in nominal operation, oriented along an axis AL12a (for the thruster 12a2 in FIG. 4) or AL12b (FIG. for the thruster 12bl in Figure 4) substantially normal to a longitudinal plane of the platform 11, is substantially parallel to a longitudinal axis ALI of the passenger 1.
• Said thrusters are also oriented so that the ejection nozzle of each of said thrusters rejects a gaseous flow in a direction opposite to that of said longitudinal axis oriented ALI from the feet to the head of the passenger 1. In this way, the thrusters "push" said passenger 1 via the platform 11.
• the main body 10a of the latter comprises support means 14 of the thrust group 12, cooperating with the platform 11, arranged to support led it push group 12 by concentrating the thrusters as centrally as possible body 10a.
• said support means 14 minimize as far as possible the distance between a median virtual axis AM10, passing through the center of gravity CG10 of the body 10a of the device 10 and each direction of gas flow ejection AL12a, AL12b by the ejection nozzle each thruster 12al, 12a2, 12bl, 12b2. This reduces the moment of inertia that the passenger must overcome to modify, with the help of his body, the body plate 10a and by Consequently, the trajectory of the propulsion device 10.
• the center of gravity CG10 of the body 10a is substantially located in the center of the thrusters of the two thrust subgroups 12a and 12b.
• the support means 14 may comprise a plate by thrust subgroup on which are mounted, by a mechanical connection of the embedding type, collars respectively surrounding the thrusters of each subgroup. In this way, the thrusters of the same thrust subgroup are held together and are oriented along parallel longitudinal axes.
• two collars 14b1 and 14b2 respectively surround the thrusters 12bl and 12b2. The two collars are also fixed on a plate 14b.
• Two collars 14al and 14a2 respectively surround the thrusters 12al and 12a2.
• the collars cooperate with a plate 14a, mostly masked in FIG. 4.
• the thickness of said plates 14a and 14b is minimized in their environments so that the thrusters of the same subgroup are closest to each other.
• the support means 14 are arranged so that the proximal portions of said plates can cooperate, so that said thrust subgroups are as close as possible.
• Said proximal portions 14m, for the plate 14b and 14f, for the plate 14a may advantageously each describe a hollow cylinder.
• the sections of said cylinders are also advantageously chosen so that one of said proximal parts penetrates the second.
• each cylinder With holes opening on both sides each cylinder along an axis normal to the axis of revolution of said proximal portions 14f and 14m, and a pin for example, it is possible to secure the two thrust subgroups.
• the thrust nozzle discharge directions may be parallel to each other and substantially normal to a longitudinal plane of the platform 11.
• the invention provides that the support means 14 can be arranged to orient the direction of ejection of gas flow by the ejection nozzle of each thruster of each thrust subgroup 12a and 12b, so that said direction of gas flow ejection describes a angle A between -10 ° and + 10 ° with a median axis of the platform 11 or the body 10a.
• the support means 14 can be arranged to orient the direction of ejection of gas flow by the ejection nozzle of each thruster of each thrust subgroup 12a and 12b, so that said direction of gas flow ejection describes a angle A between -10 ° and + 10 ° with a median axis of the platform 11 or the body 10a.
• FIG. 2B it is possible to slightly cross said ejection directions of the two subgroups 12a and 12b forming an angle resulting from the doubling of A, referenced "2.A" in FIG. 2B.
• An angle A of an absolute value of four degrees is enough to cancel the effect mentioned above, if the thrusters are not mounted counter-rotating, without penalizing the effective power of the thrust group 12.
• Other values of A could alternatively to be advocated.
• multiple holes on the proximal portions 14m and 14f of the plates 14a and 14b make it possible to choose the desired angle A.
• the plates can be oriented relative to each other in the factory by welding.
• the support means 14 of a device 10 cooperate with secondary support means 15a and 15b to cooperate with secondary thrusters 19a and 19b and maintain them in a thrust orientation substantially parallel to a longitudinal axis of the platform 11.
• the plates 14a and 14b can respectively cooperate with arms 15a and 15b, or more generally lateral extensions.
• the plates 14a and 14b have distal portions 14d, diametrically opposed to the proximal portions mentioned above. Like these, said distal portions have hollow circular sections substantially smaller or larger than those of the proximal portions 15a and 15bp of said extensions 15a and 15b.
• each extension 15a or 15b has a distal portion 15ad or 15bd arranged to encircle or more generally maintain a secondary thruster 19a or 19b.
• a secondary propellant may consist of one or more electric turbines.
• Such a technological choice makes it possible have particularly reactive secondary thrusters 19a and 19b, more than certain thermal thrusters, such as turbojets.
• the body 10a of a propulsion device advantageously comprises processing means, not only instructions of the passenger 1, but also attitude sensors and / or trajectory of said body 10a in space
• the invention provides to exploit the presence of the secondary thrusters 19a and 19b to help said passenger to maintain a course, especially if the weather is unfavorable. Indeed, a violent and irregular wind can cause the propulsion device along a laces trajectory contrary to the will of the passenger. This can be compensated using a setpoint interface, as will be explained later, but this compensation can be tedious in the long run.
• the invention thus provides for adapting the processing means present in the body 10a so that the latter develop power controls for the secondary thrusters 19a and 19b, so that they, in the absence of instructions from the passenger meaning a desired course change, maintain the current course.
• said processing means present on the body 10a, develop a power control to the secondary thruster 19b, that is to say that positioned to the right of the passenger 1, actuating said secondary thruster 19b enough to cancel this unexpected trajectory change.
• Said secondary thruster 19b is cut as soon as the nominal trajectory is recovered. In this way, the propulsion device 10 automatically maintains its current trajectory and unloads said passenger from any compensation effort.
• the choice to favor electric secondary thrusters is all the more justified by this embodiment, given the high reactivity required for such secondary thrusters 19a and 19b so that they compensate for weather hazards, without the passenger's knowledge. .
• extensions 15a and 15b respectively comprising a pair of protuberances or spacers 15p and 15s. These are positioned along an axis normal to the longitudinal axis of each extension 15a or 15b to cooperate with the platform 11.
• the latter can be fixed by screwing, said protuberances being threaded in this case. Any other mode of cooperation between the support means 14 the platform 11 could be imagined according to the invention.
• the protuberances 15p and 15s are respectively positioned on the extension 15a or 15b respectively near the distal and proximal portions of said extension.
• these protuberances make it possible to determine the relative height of the beaches 11a made on the platform 11 to accommodate the feet of the passenger 1 with respect to the center of gravity CG10 of the body 10a of the propulsion device 10.
• a tank 30 comprises a rigid or flexible envelope 33, a filling mouth 31 and a drain mouth 32. It is thus possible to supply liquid or gaseous fuel such a tank by the mouth 31.
• a fuel may be kerosene, currently commonly suitable for conventional thrusters. However, other fuels could alternatively be exploited.
• Said fuel is then delivered by said tank 30 through the drain mouth 32 arranged to cooperate with a supply duct, not shown by simplification in the figures, whose ends are respectively connected to the tank 30, more precisely to the drain mouth 32, to collect the fuel and to a collector means, also not shown in the figures, for supplying the propellants with fuel.
• a collector means serves each thermal propellant fuel. It thus cooperates by fluid connection with said thrusters and the reservoir.
• Such a tank 30 may be intended to be worn by the passenger, such as a backpack or a parachute, by means of straps or a harness. It may alternatively be fixed on the platform 11 or on the support means 14 of the thrust group.
• the envelope 33 of said tank may be advantageously flexible, such as a pre-degassed bag before being filled with fuel. Such a choice improves the comfort and safety of the passenger in case of a fall in particular and prevents any risk of defusing the fuel supply thrusters.
• the invention furthermore provides that a source of electrical energy may advantageously be carried by the main body 10a of a propulsion device 10.
• a source may consist of one or more batteries and / or photovoltaic cells, the latter serving as secondary sources for supplying electronic elements that consume little energy, such as means for processing passenger instructions and generating power control of the thrust group.
• the secondary thrusters 19a and 19b presented above will require a more substantial source such as one or more batteries, if said secondary thrusters are electric.
• a passenger 1 of a propulsion device 10 can advantageously use a man-machine interface of instructions whose primary function is to translate a gesture of said passenger 1 in a specific set.
• FIG. 6 describes an example of such a man-machine interface 60, in the form of a remote control intended to be held in the hand of the passenger 1 or of an instructor during a learning period. According to this nonlimiting example, said interface 60 is similar to a pistol type remote control.
• a trigger 61 whose stroke can be interpreted as an instruction to increase the power of the thrust group 12, when the trigger is actuated by the passenger 1 or the instructor, and slowing down said power when said trigger is gradually released by its user.
• Such an interface 60 may further comprise other members such as one or more buttons, for example pushbuttons, to possibly set start or stop instructions of the pushing group 12, to cut the power supply to this or that thruster.
• Said interface 60 may also comprise one or more sensors, such as a gyroscope, an inclinometer, or even an angular measurement sensor measuring the angle described by one of the wrists of the user whose hand holds the interface 60 to view of the longitudinal axis of the forearm concerned relative to a reference position in which the hand of said user is aligned with his forearm.
• the wrist pointing inwardly of the body of the user may mean the desire to see the device 10 pivot to the left, if said user holds the interface 60 in his right hand.
• a movement of the wrist to the outside could mean the desire to orient the trajectory of said device 10 on its right.
• the interface 60 may include an inclinometer.
• an inclination of said interface 60, to the left or to the right of its user, can then translate an orientation instruction of the trajectory of the device 10. Such an orientation instruction is then translated by secondary booster power commands. 19a and 19b previously described.
• the interface 60 described by way of example in FIG. 6, comprises electronic processing means 62 for the different information collected by the trigger 61 and other buttons and / or sensors of said interface. 60 to produce instructions interpretable by the processing means of such instructions embedded on the body 10a of the propulsion device 10.
• the interface 60 and said processing means present on the body 10a of the device 10 comprise wired communication means or advantageously wireless, for example by radio.
• Said processing means arranged to be advantageously positioned near the CG10 center of gravity of said body 10a, are arranged to generate power commands of the thrust group 12 from instructions produced by the interface 60.
• Each power control is advantageously sent to the thruster concerned by means of communication advantageously wire.
• Such communication means are not shown in the figures for the sake of simplification.
• information relating to the operation of the thrust group can be elaborated by said processing means and returned to the passenger 1 via one or more graphic interfaces 20a and / or 20b, such as screens or indicator lights.
• the body 10a of said device 10 it may be advantageous to position the body 10a of said device 10 so that the thrusters of the thrust subgroups 12a and 12b are oriented substantially horizontally. Indeed, the fuel, for example kerosene, tends to flow before the ignition of the thrusters if the latter remained vertical.
• the invention provides for this purpose, a take-off station arranged to allow the body 10a to rock when starting the thrust unit 12 and then position said body 10a so that a passenger 1 can easily take place on the beaches 11a.
• the invention provides that the thrust unit 12 can be rotatably mounted along an axis transverse to the platform 11 to allow rotation of 90 ° and thus solve the disadvantage of having to orient the body 10a if the thrust group 12 cooperates according to a recess connection with the platform 11. After starting such a rotatably mounted thrust unit 12, it would be held stationary with respect to said platform 11 as illustrated by FIGS. 2A to 2C by any means. A large number of fun applications or services are allowed through a propulsion device according to the invention.
• Accessories to further improve the playfulness or the operating conditions of such a device could also be provided: lighting, navigation means, remote control, etc.

Landscapes

• Engineering & Computer Science (AREA)
• Aviation & Aerospace Engineering (AREA)
• Chemical & Material Sciences (AREA)
• Combustion & Propulsion (AREA)
• Mechanical Engineering (AREA)
• Ocean & Marine Engineering (AREA)
• Toys (AREA)
• Structures Of Non-Positive Displacement Pumps (AREA)
• Motorcycle And Bicycle Frame (AREA)
• Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
• Magnetic Bearings And Hydrostatic Bearings (AREA)
• Vending Machines For Individual Products (AREA)
• Soil Working Implements (AREA)
• Body Structure For Vehicles (AREA)
• Emergency Management (AREA)
• Linear Motors (AREA)
• Business, Economics & Management (AREA)
• Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
• Ultra Sonic Daignosis Equipment (AREA)
• Escalators And Moving Walkways (AREA)

Applications Claiming Priority (2)

Publications (1)

Family

ID=56263910

Family Applications (2)

Family Applications After (1)

Country Status (11)

Cited By (5)

Families Citing this family (10)

Citations (11)

Family Cites Families (51)

• 2016
  • 2016-04-08 FR FR1653136A patent/FR3049931B1/fr active Active
  • 2016-05-10 FR FR1654171A patent/FR3049932B1/fr active Active
• 2017
  • 2017-04-06 WO PCT/FR2017/050825 patent/WO2017174942A1/fr active Application Filing
  • 2017-04-06 SG SG10202111205XA patent/SG10202111205XA/en unknown
  • 2017-04-06 ES ES17719865T patent/ES2939170T3/es active Active
  • 2017-04-06 WO PCT/FR2017/050829 patent/WO2017174944A1/fr active Application Filing
  • 2017-04-06 CA CA3020209A patent/CA3020209C/fr active Active
  • 2017-04-06 US US16/092,092 patent/US11453479B2/en active Active
  • 2017-04-06 EP EP21198135.2A patent/EP3950501A1/fr active Pending
  • 2017-04-06 CN CN201780035440.2A patent/CN109562832B/zh active Active
  • 2017-04-06 AU AU2017246988A patent/AU2017246988B2/en active Active
  • 2017-04-06 CN CN202111212498.4A patent/CN113830306B/zh active Active
  • 2017-04-06 IL IL262164A patent/IL262164B2/en unknown
  • 2017-04-06 EP EP17719865.2A patent/EP3439954B1/fr active Active
  • 2017-04-06 CA CA3193615A patent/CA3193615A1/fr active Pending
  • 2017-04-06 JP JP2019503791A patent/JP6978795B2/ja active Active
  • 2017-04-06 IL IL287054A patent/IL287054B2/en unknown
  • 2017-04-06 SG SG11201808862TA patent/SG11201808862TA/en unknown
• 2021
  • 2021-09-28 AU AU2021240148A patent/AU2021240148B2/en active Active
  • 2021-10-06 US US17/450,096 patent/US11840325B2/en active Active
  • 2021-10-13 JP JP2021167981A patent/JP7244028B2/ja active Active

Patent Citations (11)

Also Published As

Similar Documents

Legal Events